EP3755884B1 - Roticulating thermodynamic apparatus - Google Patents

Roticulating thermodynamic apparatus Download PDF

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Publication number
EP3755884B1
EP3755884B1 EP19707079.0A EP19707079A EP3755884B1 EP 3755884 B1 EP3755884 B1 EP 3755884B1 EP 19707079 A EP19707079 A EP 19707079A EP 3755884 B1 EP3755884 B1 EP 3755884B1
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EP
European Patent Office
Prior art keywords
rotor
chamber
port
axle
rotational axis
Prior art date
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Active
Application number
EP19707079.0A
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German (de)
English (en)
French (fr)
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EP3755884A1 (en
Inventor
Jonathan Fenton
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Fetu Ltd
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Fetu Ltd
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Priority to EP22159775.0A priority Critical patent/EP4056804A1/en
Publication of EP3755884A1 publication Critical patent/EP3755884A1/en
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02G—HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G1/00—Hot gas positive-displacement engine plants
    • F02G1/04—Hot gas positive-displacement engine plants of closed-cycle type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C9/00—Oscillating-piston machines or engines
    • F01C9/005—Oscillating-piston machines or engines the piston oscillating in the space, e.g. around a fixed point
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C11/00—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
    • F01C11/002—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/02—Arrangements of bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/08—Rotary pistons
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C9/00—Oscillating-piston machines or engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B11/00—Compression machines, plants or systems, using turbines, e.g. gas turbines
    • F25B11/02—Compression machines, plants or systems, using turbines, e.g. gas turbines as expanders
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/008—Driving elements, brakes, couplings, transmissions specially adapted for rotary or oscillating-piston machines or engines

Definitions

  • the present disclosure relates to a roticulating thermodynamic apparatus.
  • thermodynamic apparatus operable as a heat pump and/or heat engine.
  • thermodynamic expanders tend to be of a rotational type (e.g. turbines) and are typically limited to a single stage expansion ratio of 3:1.
  • the running speed of the turbine is generally higher than the running speed of the pump.
  • the pump and turbine tend to be of different types and rotate independently of one another to allow them to run at different speeds.
  • US2002/112485A1 discloses a hydraulic vane pump with a flexible band control.
  • GB2544819A discloses a fluid compression apparatus for an internal combustion engine or a fluid pump.
  • a roticulating thermodynamic apparatus having a first fluid flow section (111) comprising : a first shaft portion (118) which defines, and is rotatable about, a first rotational axis (130); a first axle (120) defining a second rotational axis (132), the first shaft portion (118) extending through the first axle (120); a first piston member (122a) provided on the first shaft portion (118), the first piston member (122a) extending from the first axle (120) towards a distal end of the first shaft portion (118); a first rotor (119) carried on the first axle (120); the first rotor (119) comprising : a first chamber (134a), the first piston member (122a) extending across the first chamber (134a); a first housing wall adjacent the first chamber (134a), a first port (114a) and second port (114b) provided in the housing wall and each in flow communication with the first chamber (134a); whereby : the first fluid flow section (111) comprising
  • the second rotational axis (132) may be substantially perpendicular to the first rotational axis (130).
  • the first rotor (119) may comprise the second chamber (134b).
  • the first piston member (122a) may extend from one side of the first axle (120) along the first shaft portion (118).
  • a second piston member (122b) may extend from the other side of the first axle (120) along the first shaft portion (118), across the second chamber (134b) to permit the first rotor (119) to pivot relative to the second piston member (122b) as the first rotor (119) rotates about the first rotational axis (130).
  • the fourth port (116b) may be in fluid communication with the first port (114a) via a second heat exchanger (306a).
  • the volumetric capacity of the first rotor first chamber (134a) may be substantially the same, less, or greater than the volumetric capacity of first rotor second chamber (134b).
  • the first shaft portion (118), first axle (120) and first piston member(s) (122a, 122b) may be fixed relative to one another.
  • the apparatus (200) may further comprise : a second rotor (219) comprising the second chamber (234b), a second shaft portion (218) rotatable about the first rotational axis (130); and the second shaft portion (218) is coupled to the first shaft portion (118) such that the first shaft portion (118) and second shaft portion (218) are rotatable together around the first rotational axis (130).
  • a second axle (220) defining a third rotational axis (232), the second shaft portion (218) extending through the second axle (220); a second piston member (222b) provided on the second shaft portion (218), the second piston member (222b) extending from the second axle (220) towards a distal end of the second shaft portion (218); the second rotor (219) carried on the second axle (220); the second piston member (222b) extending across the second chamber (234b); whereby : the second rotor (219) and second axle (220) are rotatable with the second shaft portion (218) around the first rotational axis (130); and the second rotor (219) is pivotable about the second axle (220) about the third rotational axis (232) to permit the second rotor (219) to pivot relative to the second piston member (222) as the second rotor (219) rotates about the first rotational axis (130).
  • the third rotational axis (232) may be substantially perpendicular to the first rotational axis (130).
  • the first rotor (119) may comprise :a first rotor second chamber (134b), the first piston member (122a) extending from one side of the first axle (120) along the first shaft portion (118); and a second piston member (122b) extends from the other side of the first axle (120) along the first shaft portion (118), across the first rotor second chamber (134b) to permit the first rotor (119) to pivot relative to the second piston member (122b) as the first rotor (119) rotates about the first rotational axis (130).
  • the second rotor (219) may comprise : a second rotor first chamber (234a), the second piston member (222b) extends from one side of the second axle (220) along the second shaft portion (218); and a second rotor first piston member (222a) extends from the other side of the second axle (220) along the second shaft portion (218), across the second rotor first chamber (234a) to permit the second rotor (219) to pivot relative to the second rotor first piston member (222a) as the second rotor (219) rotates about the first rotational axis (130).
  • the first rotor second chamber (134b) may be in flow communication with : a fifth port (114c) and a sixth port (114d); to thereby form part of the first fluid flow section (111), and configured for the passage of fluid between the fifth port (114c) and sixth port (114d) via the first rotor second chamber (134b); the second rotor first chamber (234a) is in flow communication with a seventh port (116c) and an eighth port (116d); to thereby form part of the second fluid flow section (115), and configured for the passage of fluid between the seventh port (116c) and eighth port (116d) via the second rotor first chamber (234b); wherein the sixth port (114d) is in fluid communication with the seventh port (116c) via the first heat exchanger (302a).
  • the eight port (116d) may be in fluid communication with the fifth port (114c) via a second heat exchanger (306a).
  • the fourth port (116b) may be in fluid communication with the first port (114a) via the second heat exchanger (306a).
  • the first chamber (134a) and second chamber (134b) of the first rotor (119) may have substantially the same volumetric capacity; the first chamber (234a) and second chamber (234b) of the second rotor (219) have substantially the same volumetric capacity; the volumetric capacity of the first rotor chambers (134a, 134b) are substantially the same, less, or greater than the volumetric capacity of the second rotor chambers (234a, 234b).
  • the first shaft portion (118) may be directly coupled to the second shaft portion (218) such that the first rotor (119) and second rotor (219) are operable to only rotate at the same speed as each other.
  • the second shaft portion (218), second axle (220) and second piston member(s) (222a, 222b) may be fixed relative to one another.
  • the first heat exchanger (302a) may be operable as a heat sink to remove heat energy from fluid passing through it.
  • the second heat exchanger (306a) may be operable as a heat source to add heat energy to fluid passing through it.
  • the first heat exchanger (302a) may comprise a chamber (810) operable to permit fluid flow between the first fluid flow section (112) and the second fluid flow section (115); and an injector (812) configured to inject a cryogenic medium into the chamber (810) such that heat energy is transferred from the fluid to the cryogenic media.
  • the first heat exchanger (302a) may be operable as a heat source to add heat energy to fluid passing through it.
  • the second heat exchanger (306a) may be operable as a heat sink to remove heat energy from fluid passing through it.
  • the first heat exchanger (302a) may comprise : a combustion chamber operable for continuous combustion.
  • the or each chamber (134a, 134b, 234a, 234b) may have an opening (36); and the or each respective piston member (122a, 122b, 222a, 222b) extends from its respective axle (20) across its corresponding chamber towards the corresponding opening (36).
  • the apparatus may further comprise : a pivot actuator operable to pivot the rotor (119, 219) about the axle (120, 220); wherein the pivot actuator comprises : a first guide feature (52) provided on the rotor (119, 219); and a second guide feature (50) provided on the housing (112); the first guide feature (52) operable to co-operate with the second guide feature (50) to pivot the rotor (119, 219) about the axle (120, 220).
  • a pivot actuator operable to pivot the rotor (119, 219) about the axle (120, 220)
  • the pivot actuator comprises : a first guide feature (52) provided on the rotor (119, 219); and a second guide feature (50) provided on the housing (112); the first guide feature (52) operable to co-operate with the second guide feature (50) to pivot the rotor (119, 219) about the axle (120, 220).
  • At least one of the first guide feature (52) and second guide feature (50) may comprise an electro-magnet operable to magnetically couple to the other of the first guide feature (52) and second guide feature (50).
  • the apparatus may further comprise : a pivot actuator operable to pivot the rotor (119, 219) about the axle (120, 220); wherein the pivot actuator comprises : a first guide feature (52) on the rotor (119, 219); and a second guide feature (50) on the housing (112); the first guide feature (52) being complementary in shape to the second guide feature (50); and one of the first or second guide features defining a path (50) which the other of the first or second guide feature (52), is constrained to follow; the other of the first or second guide feature (52) comprising a rotatable member (820) which is operable to engage the path (50) and rotate as it moves along the path (50).
  • a pivot actuator operable to pivot the rotor (119, 219) about the axle (120, 220); wherein the pivot actuator comprises : a first guide feature (52) on the rotor (119, 219); and a second guide feature (50) on the housing (112); the first guide feature (52) being complementary in shape to the
  • the heat source may further comprises a substance passing through a duct (303) in the first heat exchanger 302a, wherein the apparatus (1000) provides cooling to the substance.
  • the fluid passing through the apparatus may comprise air.
  • the apparatus comprises a motor (308) coupled to the first shaft portion 118 configured to drive the rotor (119) around the first rotational axis (130).
  • the motor (308) may be reversible, such that when the motor is configured to drive the rotor (119) around the first rotational axis (130) in a first direction, the first heat exchanger (302a) is operable to act as a heat source to transfer heat from the substance to the fluid, and wherein when the motor is configured to drive the rotor (119) around the first rotational axis (130) in a second direction, opposite to the first direction, the first heat exchanger (302a) is operable to act as a heat sink to transfer heat from the fluid to the substance.
  • the second guide feature (550) may comprises a slewing ring (527) configured to hold at least part of a bearing (529) that is coupled with the housing.
  • the first guide feature (552) may comprise a stylus configured to be received in the slewing ring (527).
  • a roticulating thermodynamic apparatus having a first fluid flow section (111) comprising : a first shaft portion (118) which defines, and is rotatable about, a first rotational axis (130); a first axle (120) defining a second rotational axis (132), the first shaft portion (118) extending through the first axle (120); a first piston member (122a) provided on the first shaft portion (118), the first piston member (122a) extending from the first axle (120) towards a distal end of the first shaft portion (118); a first rotor (119) carried on the first axle (120); the first rotor (119) comprising : a first chamber (134a), the first piston member (122a) extending across the first chamber (134a); a first casing wall adjacent the first chamber (134a), a first port (114a) and second port (114b) provided in the housing wall and each in flow communication with the first chamber (134a); whereby : the first fluid flow section (111) comprising
  • an apparatus operable to displace and expand fluid which may be configured as heat pump to remove heat from a system (e.g. a refrigerator) or configured as a heat engine to extract work from a working fluid in order to provide a rotational output.
  • the displacement section (e.g. pump) and expansion section (e.g. turbine) of the present device can sustain their optimal efficiency at near identical speeds and be subject to a single set of mechanical constraints by virtue of being housed within a common device.
  • arrangements of the present disclosure may be substantially thermodynamically ideal.
  • the apparatus may comprise a core element having linked displacement and expansion chambers which are defined by walls of a single common rotor.
  • the rotor is pivotable relative to a rotatable piston.
  • the core elements may be described as a 'roticulator' since the rotor of the present disclosure is operable to simultaneously 'rotate' and 'articulate', for example as described in PCT Application PCT/GB2016/052429 (Published as WO2017/089740 ) .
  • heat engine or heat pump which comprises a 'roticulating apparatus' .
  • Roticulation and the roticulating concept hence describe a device in which a single body (e.g. a rotor) rotates whilst simultaneously articulating, describing a 3D spatial movement which can be used to perform volumetric 'work' in conjunction and translation with rotation.
  • a single body e.g. a rotor
  • the apparatus offers absolute management and control of multiple volumetric chambers within a single order of mechanical constraints/losses. Given this high ratio of volumetric chambers over mechanical losses the efficiency of the device is of a high order when compared to conventional devices.
  • this disclosure describes a device capable of both positive displacement and absolute evacuation of its working volumes, such is characteristic of an 'ideal' expander/compressor/pump, offering a high expansion/compression ratio many orders beyond conventional devices.
  • the apparatus offers the highly desirable characteristic of a single device operable to simultaneously perform the action of expansion of a working fluid as well as compression and/or displacement of the same working fluid.
  • a heat engine according to the present disclosure may operate with a lower heat differential, utilising lower quality heat than examples of the related art.
  • first fluid flow section and second fluid flow sections are linked, a heat pump according to the present disclosure is inherently more efficient than an example of the related art as expansion of the fluid is utilised to drive the displacement/pump/compressing section, thereby requiring less external input from a motor.
  • apparatus may efficiently operate over a wide range of conditions, thereby allowing the device to produce outputs with input conditions which would not provide sufficient energy for examples of the related art to operate.
  • thermodynamic apparatus operable as a heat pump and/or heat engine.
  • the apparatus is suitable for use as part of a fluid working apparatus operable as a heat pump and/or a heat engine.
  • Core elements of the apparatus are described as well as non-limiting examples of applications in which the apparatus may be employed.
  • fluid is intended to have its normal meaning, for example : a liquid, gas, vapour, or a combination of liquid, gas and/or vapour, or material behaving as a fluid.
  • Figure 1 shows a part exploded view of a core 10 part of an apparatus according to the present disclosure.
  • the core 10 comprises a housing 12 and rotor assembly 14.
  • Figure 2 shows an alternative example of a housing 12 when it is closed around the rotor assembly 14.
  • the housing 12 is divided into two parts 12a, 12b which close around the rotor assembly 14.
  • the housing may be fabricated from more than two parts, and/or split differently to that shown in Figure 1 .
  • the rotor assembly 14 comprises a rotor 16, a shaft 18, an axle 20 and a piston member 22.
  • the housing 12 has a wall 24 which defines a cavity 26, the rotor 16 being rotatable and pivotable within the cavity 26.
  • the shaft 18 defines, and is rotatable about, a first rotational axis 30.
  • the axle 20 extends around the shaft 18.
  • the axle extends at an angle to the shaft 18.
  • the axle defines a second rotational axis 32.
  • the axle 20 defines the second rotational axis 32, and the shaft 18 extends through the axle 20 at an angle to the axle 20.
  • the piston member 22 is provided on the shaft 18.
  • the apparatus is provided with two piston members 22, i.e. a first and second piston member 22.
  • the rotor 16 also defines two chambers 34a,b, one diametrically opposite the other on either side of the rotor 16.
  • each chamber 34 may be provided as a compression chamber.
  • each chamber 34 may be provided as a displacement chamber.
  • each chamber 34 may be provided as an expansion or metering chamber.
  • piston member 22 may in fact be one piece that extends all of the way through the rotor assembly 14, this arrangement effectively means each chamber 34 is provided with a piston member 22. That is to say, although the piston member 22 may comprise only one part, it may form two piston members sections 22, one on either side of the rotor assembly 14.
  • a first piston member 22 extends from one side of the axle 20 along the shaft 18 towards one side of the housing 12, and a second piston member 22 extends from the other side of the axle 20 along the shaft 18 towards the other side of the housing 12.
  • the rotor 16 comprises a first chamber 34a having a first opening 36 on one side of the rotor assembly 14, and a second chamber 34b having a second opening 36 on the other side of the rotor assembly 14.
  • the rotor 16 is carried on the axle 20, the rotor 16 being pivotable relative to the axle 20 about the second rotational axis 32.
  • the piston member 22 extends from the axle 20 across the chambers 34a,b towards the openings 36.
  • a small clearance is maintained between the edges of the piston member 22 and the wall of the rotor 16 which defines the chamber 34.
  • the clearance may be small enough to provide a seal between the edges of the piston member 22 and the wall of the rotor 16 which defines the chamber 34.
  • sealing members may be provided between the piston members 22 and the wall of the rotor 16 which defines the chamber 34.
  • the chambers 34 are defined by side walls (i.e. end walls of the chambers 34) which travel to and from the piston members 22, the side walls being joined by boundary walls which travel past the sides of the piston member 22. That is to say, the chambers 34 are defined by side/end walls and boundary walls provided in the rotor 16.
  • the rotor 16 is rotatable with the shaft 18 around the first rotational axis 30, and pivotable about the axle 20 about the second rotational axis 32.
  • This configuration results in the first piston member 22 being operable to travel (i.e. traverse) from one side of the first chamber 34a to an opposing side of the first chamber 34a as the rotor 16 rotates about the first rotational axis 30.
  • the rotor 16 is rotatable with the shaft 18 around the first rotational axis 30, and the rotor 16 is pivotable about the axle 20 about the second rotational axis 32, during operation there is a relative pivoting (i.e.
  • the apparatus is configured to permit a controlled pivoting motion of the rotor 16 relative to the first piston member 22 as the rotor 16 rotates about the first rotational axis 30.
  • the configuration also results in the second piston member 22 being operable to travel (i.e. traverse) from one side of the second chamber 34b to an opposing side of the second chamber 34b as the rotor 16 rotates about the first rotational axis 30.
  • the rotor 16 is rotatable with the shaft 18 around the first rotational axis 30, and the rotor 16 is pivotable about the axle 20 about the second rotational axis 32, during operation there is a relative pivoting (i.e. rocking) motion between the rotor 16 and both piston members 22 as the rotor 16 rotates about the first rotational axis 30. That is to say, the apparatus is configured to permit a controlled pivoting motion of the rotor 16 relative to both piston members 22 as the rotor 16 rotates about the first rotational axis 30.
  • the relative pivoting motion is induced by a pivot actuator, as described below.
  • the mounting of the rotor 16 such that it may pivot (i.e. rock) relative to the piston members 22 means that the piston members 22 provide a moveable division between two halves of the or each chambers 34a,b to form sub-chambers 34a1, 34a2, 34b1, 34b2 within the chambers 34a,34b.
  • the volume of each sub chamber 34a1, 34a2, 34b1 and 34b2 varies depending on the relative orientation of the rotor 16 and piston members 22.
  • the rotor 16 When the housing 12 is closed about the rotor assembly 14, the rotor 16 is disposed relative to the housing wall 24 such that a small clearance is maintained between the chamber opening 34 over the majority of the wall 24.
  • the clearance may be small enough to provide a seal between the rotor 16 and the housing wall 24.
  • sealing members may be provided in the clearance between the housing wall 24 and rotor 16.
  • Ports are provided for the communication of fluid to and from the chambers 34a,b.
  • the housing 12 may comprise an inlet port 40 for delivering fluid into the chamber 34, and an exhaust/outlet port 42 for expelling fluid from the chamber 34.
  • the ports 40, 42 extend through the housing and open onto the wall 24 of the housing 12.
  • the inlet and outlet/exhaust ports 40, 42 are shown in different orientations in Figure 1 and Figure 2 .
  • the flow direction defined by each port is at an angle to the first rotational axis 30.
  • the flow direction defined by each port is parallel to the first rotational axis 30.
  • the ports 40, 42 may have the same flow areas. In other examples the ports 40, 42 may have different flow areas.
  • bearing arrangement 44 for supporting the ends of the shaft 18. This may be of any conventional kind suitable for the application.
  • the ports 40, 42 may be sized and positioned on the housing 12 such that, in operation, when respective chamber openings 36 move past the ports 40, 42, in a first relative position the openings 36 are aligned with the ports 40, 42 such that the chamber openings are fully open, in a second relative position the openings 36 are out of alignment such that the openings 36 are fully closed by the wall 24 of the housing 12, and in an intermediate relative position, the openings 36 are partly aligned with the ports 40, 42 such that the openings 36 are partly restricted by the wall of the housing 24.
  • the ports 40,42 may be sized and positioned on the housing 12 such that, in operation, in a first range (or set) of relative positions of the ports 40,42 and the respective rotor openings 36, the ports 40,42 and rotor openings 36 are out of alignment such that the openings 36 are fully closed by the wall 24 of the housing 12 to prevent fluid flow between the sub-chambers 34a1, 34a2 and their respective port(s) 40,42, and to prevent fluid flow between the sub-chambers 34b1, 34b2 and their respective port(s) 40,42.
  • the openings 36 are at least partly aligned with the ports 40,42 such that the openings 36 are at least partly open to allow fluid to flow between the sub chambers of chamber(s) 34a,b and their respective port(s) 40,42.
  • the sub-chambers are operable to increase in volume at least when in fluid communication with an inlet port (to allow for fluid flow into the sub-chamber), and the sub-chambers are operable to decrease in volume at least when in fluid communication with an outlet port (to allow for fluid flow out of the sub-chamber).
  • the placement and sizing of the ports may vary according to the application (i.e. whether used as part of a fluid pump apparatus, fluid displacement apparatus, fluid expansion apparatus) to facilitate best possible operational efficiency.
  • the port locations herein described and shown in the figures is merely indicative of the principle of media (e.g. fluid) entry and exit.
  • the inlet ports and outlet ports may be provided with mechanical or electro-mechanical valves operable to control the flow of fluid/media through the ports 40,42.
  • the apparatus may comprise a pivot actuator.
  • a non-limiting example of the pivot actuator is illustrated in Figure 3 , which corresponds to that shown in Figures 1, 2 .
  • the pivot actuator may comprise any suitable form of guide means configured to control the pivoting motion of the rotor.
  • the pivot actuator may comprise an electromagnetic arrangement configured to control the pivoting motion of the rotor. That is to say the pivot actuator may comprise a first guide feature 52 provided on the rotor 119, 219, and a second guide feature 50 provided on the housing 112, the first guide feature 52 operable to co-operate with the second guide feature 50 to pivot the rotor about the axle. At least one of the first guide feature 52 and second guide feature 50 comprises an electro-magnet operable to magnetically couple to the other of the first guide feature 52 and second guide feature 50.
  • the pivot actuator is operable (i.e. configured) to pivot the rotor 16 about the axle 20. That is to say, the apparatus may further comprise a pivot actuator operable (i.e. configured) to pivot the rotor 16 about the second rotational axis 32 defined by the axle 20.
  • the pivot actuator may be configured to pivot the rotor 16 by any angle appropriate for the required performance of the apparatus. For example the pivot actuator may be operable to pivot the rotor 16 through an angle of substantially about 60 degrees.
  • the pivot actuator may comprise, as shown in the examples, a first guide feature on the rotor 16, and may have a second guide feature on the housing 12.
  • the pivot actuator may be provided as a mechanical link between the rotor 16 and housing 12 configured to induce a controlled relative pivoting motion of the rotor 16 relative to the piston member 22 as the rotor 16 rotates about the first rotational axis 30. That is to say, it is the relative movement of the rotor 16 acting against the guide features of the pivot actuator which induces the pivoting motion of the rotor 16.
  • the first guide feature is complementary in shape to the second guide feature.
  • One of the first or second guide features define a path which the other of the first or second guide members features is constrained to follow as the rotor rotates about the first rotational axis 30.
  • the path perhaps provided as a groove, has a route configured to induce the rotor 16 to pivot about the axle 20 and axis 32. This route also acts to set the mechanical advantage between the rotation and pivoting of the rotor 16.
  • a stylus 52 is provided on the rotor 16 and, as shown in Figures 1 , 3 , a guide groove 50 is provided in the housing 12. That is to say, the guide path 50 may be provided on the housing, and the other guide feature, the stylus 52 may be provided on the rotor 16.
  • a rotor assembly 14 akin to the example shown in Figures 1 , 3 is shown in Figures 4 to 7 .
  • a stylus 52 on the rotor 16 for engagement with the guide groove 50 on the housing 12.
  • the rotor 16 may be substantially spherical. As shown, the rotor 16 may be, at least in part, substantially spherical.
  • Figure 4 shows the entire rotor assembly 14 with shaft 18, axle 20 and piston member 22 fitted.
  • Figure 5 shows the rotor 16 by itself, and a cavity 60 which extends through the rotor 14 and is configured to receive the axle 20.
  • Figure 6 shows a view looking along the first rotational axis 30 on Figure 6, and Figure 7 the same view as shown in Figure 6 looking down the opening 36 which defines the chamber 34 of the rotor 14.
  • Figure 8 shows a perspective view of the axle 20 having the passage 62 for receiving the axle 18 and piston member 22.
  • the axle 20 is substantially cylindrical.
  • Figure 9 shows an example configuration of the shaft 18 and piston member 22.
  • the shaft 18 and piston member 22 may be integrally formed, as shown in Figure 10 , or may be fabricated from a number of parts.
  • the piston member 22 is substantially square or rectangular in cross section.
  • the shaft 18 may comprise cylindrical bearing regions which extend from the piston member 22 in order to seat on the bearing arrangement 44 of the housing 12, and hence permit rotation of the shaft 18 around the first rotational axis 30.
  • Figure 10 shows the shaft 18 and piston member 22 assembled with the axle 20. They may be formed as an assembly, as described above, or they may be integrally formed as one, perhaps by casting or forging.
  • the axle 20 may be provided substantially at the centre of the shaft 18 and piston member 22. That is to say, the axle 20 may be provided substantially halfway between the two ends of the shaft 18. When assembled, the shaft 18, axle 20 and piston member 22 may be fixed relative to one another.
  • the axle 20 may be substantially perpendicular to the shaft and piston member 22, and hence the second rotational axis 32 may be substantially perpendicular to the first rotational axis 30.
  • the piston members 22 are sized to terminate proximate to the wall 24 of the housing 12, a small clearance being maintained between the end of the piston members 22 and the housing wall 24.
  • the clearance may be small enough to provide a seal between the piston members 22 and the housing wall 24.
  • sealing members may be provided in the clearance between the housing wall 24 the piston members 22.
  • FIG. 11 Further examples of a guide groove 50 are shown in cross section in Figures 11, 12 which correspond to the example of Figure 1 .
  • the guide groove 50 is substantially circular (i.e. with no inflexions).
  • the rotor 14 may be provided in one or more parts which are assembled together around the shaft 18 and axle 20 assembly.
  • the rotor 16 may be provided as one piece, whether integrally formed as one piece or fabricated from several parts to form one element, in which case the axle 20 may be slid into the cavity 60, and then the shaft 18 and piston member 22 slid into a passage 62 formed in the axle 20, and then fixed together.
  • a small clearance may be maintained between the axle 20 and bore of the cavity 60 of rotor 16.
  • the clearance may be small enough to provide a seal between the axle 20 and the rotor 16 bore of the cavity 60.
  • sealing members may be provided in the clearance between the axle 20 and rotor 16 bore of the cavity 60.
  • the guide path 50 describes a path around (i.e. on, close to, and/or to either side of) a first circumference of the housing.
  • the plane of the first circumference overlays, or is aligned with, the plane described by the second rotational axis 32 as it rotates about the first rotational axis 30.
  • Figure 13 shows a half housing split along the horizontal plane upon which the first rotational axis 30 sits.
  • the guide path 50 comprises at least a first inflexion point 70 (on one side of the housing 12) to direct the path away from a first side of the plane of the second rotational axis 32, then toward a second side of the plane of the second rotational axis 32, and a second inflexion point 72 (on the opposite side of the housing) to direct the path 50 away from the second side of the plane of the second rotational axis 32 and then back toward the first side of the plane of the second rotational axis 32.
  • the path 50 is not aligned with the plane of the second rotational axis 32, but rather oscillates from side to side of the plane of the second rotational axis 32. That is to say, the path 50 does not sit on the plane of the second rotational axis 32, but defines a sinusoidal route between either side of the plane of the second rotational axis 32.
  • the path 50 may be offset from the second rotational axis 32.
  • the distance which the guide path extends from an inflexion 70,72 on one side of the plane of the second rotational axis 32 to an inflexion 70,72 on the other side of the plane of the second rotational axis 32 defines the relationship between the pivot angle of the rotor 16 about the second rotational axis 32 and the angular rotation of the shaft 18 about the first rotational axis 30.
  • the number of inflexions 70,72 defines a ratio of number of pivots (e.g. compression, expansion, displacement cycles etc) of the rotor 16 about the second rotational axis 32 per revolution of the rotor 16 about the first rotational axis 30.
  • the trend of the guide path 50 defines a ramp, amplitude and frequency of the rotor 16 about the second rotational axis 32 in relation to the rotation of the first rotational axis 30, thereby defining a ratio of angular displacement of the chambers 34 in relation to the radial reward from the shaft (or vice versa) at any point.
  • the attitude of the path 50 directly describes the mechanical ratio/relationship between the rotational velocity of the rotor and the rate of change of volume of the rotor chambers 34a, 34b. That is to say, the trajectory of the path 50 directly describes the mechanical ratio/relationship between the rotational velocity of the rotor 16 and the rate of pivot of the rotor 16.
  • the rate of change and extent of displacement in chamber volume in relation to the rotational velocity of the rotor assembly 14 is set by the severity of the trajectory change (i.e. the inflexion) of the guide path.
  • the profile of the groove can be tuned to produce a variety of displacement versus compression characteristics, as combustion engines for petrol, diesel (and other fuels), pump and expansion may require different characteristics and/or tuning during the operational life of the rotor assembly. Put another way, the trajectory of the path 50 can be varied.
  • the guide path 50 provides a "programmable crank path" which may be pre-set for any given application of the apparatus. That is to say, the route may be optimised to meet the needs of the application. Put another way, the guide path may be programmed to suit differing applications.
  • the features defining the guide path 50 may be moveable to allow adjustment of the path 50, which may provide dynamic adjustment of the crank path while the apparatus is in operation. This may allow for tuning of rate and extent of the pivoting action of the rotor about the second rotational axis to assist with controlling performance and/or efficiency of the apparatus. That is to say, an adjustable crank path would enable variation of the mechanical ratio/relationship between the rotational velocity of the rotor and the rate of change or extent of displacement of the volume of the rotor chambers 34a, 34b.
  • the path 50 may be provided as a channel element, or the like, which is fitted to the rotor 12 and rotor housing 16, and which can be moved and/or adjusted, in part or as a whole, relative to the rotor 12 and rotor housing 16.
  • path 50 and inflexions 70, 72 define the rate of change of displacement of the rotor 16 relative to the piston 22, enabling a profound effect on the mechanical reward between the rotation and pivoting of the rotor 16.
  • Figure 14 shows another non limiting example of a rotor 16, akin to that shown in Figures 4 to 7 .
  • Bearing lands 73 are shown for receiving a bearing assembly (e.g. a roller bearing arrangement), or providing a bearing surface, to carry the rotor 16 on the axle 20.
  • a "cut out" feature 74 provided as a cavity in a non-critical region of the rotor, which lightens the structure (i.e. provides a weight saving feature) and provides a land to grip/clamp/support the rotor 16 during manufacture.
  • An additional land 75 adjacent the stylus 52 may also be provided to grip/clamp/support the rotor 16 during manufacture.
  • the stylus 52 is provided as a roller bearing, rotatable about an axis perpendicular to axis 32.
  • the bearing engages with, and runs along, the guide path 50, rotating as it moves along the track, thereby minimising friction between the guide member and track features.
  • Figures 15 , 16 and 19 to 24 illustrate how the rotor apparatus of Figures 1 to 14 , 17, 18 may be adapted to operate as a heat pump or heat engine. Any of the features described with reference to Figures 1 to 14 , 17, 18 may be included in the arrangements of Figures 15 , 16 and 19 to 24 . Common terminology is used to identify common features, although in order to distinguish between features of the examples, alternative reference numerals are used as appropriate.
  • Figure 15 illustrates an apparatus 100 according to the present disclosure arranged as a closed loop heat pump, for example a refrigeration unit.
  • the apparatus 100 comprises a first shaft portion 118 (akin to shaft 18) which defines, and is rotatable about, a first rotational axis 130 (akin to rotational axis 30).
  • a first axle 120 (akin to axle 20) defines a second rotational axis 132 (akin to rotational axis 32), the first shaft portion 118 extending through the first axle 120.
  • the second rotational axis 132 is substantially perpendicular to the first rotational axis 130.
  • a first piston member 122a (akin to first piston member 22) is provided on the first shaft portion 118, the first piston member 122a extending from the first axle 120 towards a distal end of the first shaft portion 118.
  • a first rotor 119 (akin to rotor 16 in Figures 1 to 14 , 17, 18 ) is carried on the first axle 120.
  • a housing 112 (akin to housing 12) is provided around the rotor 119 assembly.
  • the first rotor 119 comprises a first chamber 134a (akin to first chamber 34a), the first piston member 122a extending across the first chamber 134a.
  • a wall of the housing 112 is provided adjacent the first chamber 134a.
  • first port 114a Provided in the wall of the housing 112, and adjacent the first chamber 134a, is a first port 114a and a second port 114b (i.e akin to ports 40, 42).
  • the ports 114a, 114b are in flow communication with the first chamber 134a, and are operable as flow inlets/outlets.
  • the first chamber 134a is divided into sub-chambers 134a1, 134a2 (akin to sub-chambers 34a1, 34a2), each on opposite sides of the piston 122a. Hence at any one time, the ports 114a, 114b may be in flow communication with one of the sub-chambers 134a1, 134a2, but not both.
  • the first rotor 119 comprises a second chamber 134b (akin to second chamber 34b).
  • a wall of the housing 112 is provided adjacent the second chamber 134b.
  • the housing 112 comprises a third port 116a and fourth port 116b, which are in flow communication with the second chamber 134b.
  • the ports 116a, 116b are in flow communication with the first chamber 134b, and are operable as flow inlets/outlets.
  • the second chamber 134b is divided into sub-chambers 134b1, 134b2 (akin to sub-chambers 34b1, 34b2), each on opposite sides of the piston 122b. Hence at any one time, the ports 116a, 116b may be in flow communication with one of the sub-chambers 134b1, 134b2, but not both.
  • the first piston member 122a extends from one side of the first axle 120 along the first shaft portion 118, and a second piston member 122b (akin to second piston member 22) extends from the other side of the first axle 120 along the first shaft portion 118, across the second chamber 134b.
  • the arrangement is configured to permit relative pivoting motion between the first rotor 119 and the second piston member 122b as the first rotor 119 rotates about the first rotational axis 130.
  • the first shaft portion 118, first axle 120 and first piston member(s) 122a, 122b may be fixed relative to one another.
  • first rotor 119 and first axle 120 are rotatable with the first shaft portion 118 around the first rotational axis 130, and the first rotor 119 is pivotable about the axle 120 about the second rotational axis 132 to permit relative pivoting motion between the first rotor 119 and the first piston member 122a as the first rotor 119 rotates about the first rotational axis 130.
  • the second port 114b is in fluid communication with the third port 116a via a first duct/conduit 300a which comprises a first heat exchanger 302a.
  • the first heat exchanger 302a is operable to remove heat energy from working fluid passing through it. That is to say, the first heat exchanger 302a is a heat sink for the working fluid (i.e. a heat sink for the medium or media flowing through the system).
  • a first section 300a1 of duct 300a connects the second port 114b to the first heat exchanger 302a, and a second section 300a2 of duct 300a connects the first heat exchanger 302a to third port 116a. That is to say, a fluid in a duct/conduit 300a may pass through the first heat exchanger 302.
  • first chamber 134a heat exchanger 302a and second chamber 134b are arranged in flow series.
  • the fourth port 116b is in fluid communication with the first port 114a via a second duct (or conduit) 304a which comprises a second heat exchanger 306a.
  • the second heat exchanger 306a is operable to add heat energy from working fluid passing through it. That is to say, the second heat exchanger 306a is a heat source for the working fluid (i.e. a heat source for the medium or media flowing through the system).
  • the first heat exchanger 302a may be provided as any suitable heat sink (for example in thermal communication with a volume to be heated, a river, ambient air etc).
  • the second heat exchanger 306a may comprise or be in thermal communication with any suitable heat source (for example, a volume to be cooled, the internal air of a food store etc).
  • a first section 304a1 of duct 304a connects the fourth port 116b to the second heat exchanger 306a, and a second section 304a2 of duct 304a connects the second heat exchanger 306a to the first port 114a.
  • a motor 308 is coupled to the first shaft portion 118 to drive the rotor 119 around the first rotational axis 130.
  • the first chamber 134a and piston 122a hence provide a first fluid flow section 111, which in this example are operable as a compressor or displacement pump.
  • the first fluid flow section 111 is configured for the passage of fluid between the first port 114a and second port 114b via the first chamber 134a.
  • the second chamber 134b and piston 122b hence provide a second fluid flow section 115, which in this example are operable as a metering section or expansion section.
  • the second fluid flow section 115 is configured for the passage of fluid between the third port 116a and fourth port 116b via the second chamber 134.
  • the volumetric capacity of the first rotor second chamber 134b may be substantially the same, less, or greater than the volumetric capacity of the first rotor first chamber 134a.
  • the volumetric capacity of the second fluid flow section 115 may be the same, less, or greater than the volumetric capacity of the first fluid flow section 111.
  • the volumetric capacity of the first rotor second chamber 134b may be at most half the volumetric capacity of the first rotor first chamber 134a.
  • the volumetric capacity of the first rotor second chamber 134b may be at least twice the volumetric capacity of the first rotor first chamber 134a.
  • this provides an expansion ratio within the confines of a single device (for example as shown in Figure 17 ).
  • first rotor first chamber 134a as a different width than the first rotor second chamber 134b, with the first piston 122a consequentially having a different width than the second piston 122b.
  • the pistons will pivot, and hence travel, to the same extent around the second rotational axis 132, the volume of the chambers 134a, 134b and swept volume of the pistons 122a, 122b will differ.
  • the different volumes may be achieved by providing the first rotor first chamber 134a as wider than the first rotor second chamber 134b, with the first piston 122a consequentially being wider than the second piston 122b.
  • the pistons will pivot, and hence travel, to the same extent around the second rotational axis 132, the volume of the chamber 134a will be greater than the volume of chamber 134b, and hence the swept volume of the piston 122a will be greater than piston 122b.
  • the fluid may be a refrigerant fluid or other media, for example, but not limited to, Ethanol, R22 or Super saturated CO 2 .
  • the working fluid may not be consumed or rendered inoperable after each cycle. That is to say, for the majority of its operation the same fixed volume of working fluid will remain and continually cycle around the system.
  • the working fluid may be partly or wholly replaced during operation of the device (for example during each cycle, or after a predetermined number of cycles).
  • first fluid flow section 111 in this example a displacement/compressor/pump section
  • second fluid flow section 115 in this example an metering/expansion section
  • the rotation of the rotor 119 is driven both by the motor and the metering/expansion of the fluid in the second chamber 134b (i.e. in sub-chambers 134b1, 134b2).
  • the configuration of the device of the present disclosure recovers some of the energy from the expansion phase to partly drive the rotor 119.
  • the working fluid enters the sub-chamber 134a1 via port 114a.
  • the working fluid is then pumped (e.g. compressed) by the action of the piston 122a, driven by the motor 308, in the sub-chamber 134a and exits via the second port 114b.
  • working fluid is being drawn into the sub-chamber 134a1, working fluid is being exhausted from sub-chamber 134a2 through the second port 114b.
  • working fluid is being drawn into sub-chamber 134a2 through the first port 114b.
  • the working fluid travels along duct 300a2 and enters the sub-chamber 134b1 of the rotor via the third port 116a where it its pressure is restrained and the working fluid is metered into duct 304a via the fourth port 116b.
  • the working fluid is exhausted from the sub-chamber 134b1 via the fourth port 116b, and more working fluid enters the sub-chamber 134b2 via the third port 116a where it expands.
  • sequential expansion of the working fluid in the rotor sub-chambers 134b1, 134b2 induces a force to thereby (at least in part) cause pivoting of the rotor about its second rotational axis, and to cause rotation of the rotor about its first rotational axis.
  • This force is in addition to that provided by the motor 308.
  • working fluid then travels from the second chamber 134b along duct 304a1 and enters the second heat exchanger 306a, which in this example is configured as a heat source.
  • the working fluid absorbs heat from the heat source and then leaves the second heat exchanger 306a and travels along duct 304a2 before entering the first chamber 134a to re-start the cycle.
  • Figure 16 illustrates another example of a closed loop heat pump, for example a refrigeration unit.
  • This example includes many features in common with, or equivalent to, the example of Figure 15 , and are hence referred to with the same reference numerals.
  • the apparatus 200 comprises a first fluid flow section 111 which, akin to the example of Figure 15 may be operable as a compressor or displacement pump.
  • the first fluid flow section 111 has a first port 114a and a second port 114b, which are operable as flow inlets/outlets.
  • the second fluid flow section 115 also comprises a second fluid flow section 115 which, akin to the example of Figure 15 , may be operable as a metering section or expansion section.
  • the second fluid flow section 115 has a third port 116a and a fourth port 116b, which are operable as flow inlets/outlets.
  • the apparatus 200 comprises a first shaft portion 118 which defines and is rotatable about a first rotational axis 130.
  • a first axle 120 defines a second rotational axis 132, the first shaft portion 118 extending through the first axle 120.
  • the second rotational axis 132 is substantially perpendicular to the first rotational axis 130.
  • a first piston member 122a is provided on the first shaft portion 118, the first piston member 122a extending from the first axle 120 towards a distal end of the first shaft portion 118.
  • a first rotor 119 is carried on the first axle 120.
  • the first rotor 119 comprises a first chamber 134a, the first piston member 122a extending across the first chamber 134a.
  • the first displacement outlet 113a and first displacement inlet 114a are in flow communication with the first chamber 134a.
  • the first shaft portion 118, first axle 120 and first piston member(s) 122a, 122b may be fixed relative to one another.
  • the first rotor 119 comprises a second chamber 134b.
  • the first piston member 122a extends from one side of the first axle 120 along the first shaft portion 118 through the first chamber 134a to define sub-chambers 134a1, 134a2, and a second piston member 122b extends from the other side of the first axle 120 along the first shaft portion 118, across the second chamber 134b to define sub-chambers 134b1, 134b2.
  • the arrangement is configured to permit relative pivoting motion between the first rotor 119 and the second piston member 122b as the first rotor 119 rotates about the first rotational axis 130.
  • the first rotor 119 and first axle 120 are rotatable with the first shaft portion 118 around the first rotational axis 130, and the first rotor 119 is pivotable about the axle 120 about the second rotational axis 132 to permit relative pivoting motion between the first rotor 119 and the first piston member 122a and second piston member 122b as the first rotor 119 rotates about the first rotational axis 130.
  • the apparatus 200 further comprises a second shaft portion 218 rotatable about the first rotational axis 130 and coupled to the first shaft portion 118 such that the first shaft portion 118 and second shaft portion 218 are rotatable together around the first rotational axis 130.
  • a second axle 220 defines a third rotational axis 232, the second shaft portion 218 extending through the second axle 220.
  • the third rotational axis 232 is substantially perpendicular to the first rotational axis 130 and parallel to the second rotational axis 132 of the first rotor, and would hence extend out of/into the page as shown in Figure 16 .
  • a second rotor 219 is carried on the second axle 220.
  • the first shaft portion 118 is directly coupled to the second shaft portion 218 such that the first rotor 119 and second rotor are operable to only rotate at the same speed as each other.
  • a second housing 212 (akin to housing 12) is provided around the second rotor 219.
  • the second rotor 219 comprises a first chamber 234a and a second chamber 234b.
  • a second piston member 222b is provided on the second shaft portion 218, the second piston member 222b extending from the second axle 220 across the second chamber 234b towards a distal end of the second shaft portion 218 to define sub-chambers 234b1, 234b2.
  • the second piston member 222b extends from one side of the second axle 220 along the second shaft portion 218.
  • a second rotor first piston member 222a extends from the other side of the second axle 220 along the second shaft portion 218, across the first chamber 234a to define sub-chambers 234a1, 234a2.
  • the arrangement is configured to permit relative pivoting motion between the second rotor 219 and the first and second piston members 222a, 222b as the second rotor 219 rotates about the first rotational axis 130.
  • the second shaft portion 218, second axle 220 and second piston member(s) 222a, 222b may be fixed relative to one another.
  • the third port 116a and fourth port 116b are in flow communication with the second chamber 234b, the third port 116a and fourth port 116b being provided in a wall of housing 212 of the second rotor.
  • the second rotor 219 and second axle 220 are rotatable with the second shaft portion 218 around the first rotational axis 130, and the second rotor 219 is pivotable about the second axle 220 about the third rotational axis 232 to permit relative pivoting motion between the second rotor 219 and the first and second piston members 222a, 222b as the second rotor 219 rotates about the first rotational axis 130.
  • the second port 114b of the first rotor 119 is in fluid communication with the third port 116a of the second rotor 219 via a first duct/conduit 300a which comprises a first heat exchanger 302a.
  • the first heat exchanger 302a is operable to remove heat energy from working fluid passing through it (i.e. is a heat sink ).
  • a first section 300a1 of duct 300a connects the second port 114b to the first heat exchanger 302a, and a second section 300a2 of duct 300a connects the first heat exchanger 302a to the third port 116a.
  • the first rotor second chamber 134b is in flow communication with a fifth port 114c and a sixth port 114d provided in a wall of the first housing 112, such that the arrangement is configured for the passage of fluid between the fifth port 114c and sixth port 114d via the first rotor second chamber 134b.
  • the second rotor first chamber 234a is in flow communication with a seventh port 116c and an eighth port 116d provided in a wall of the second housing 212, such that the arrangement is configured for the passage of fluid between the seventh port 116c and eighth port 116d via the second rotor first chamber 234a.
  • the sixth port 114d of the first rotor 119 is in fluid communication with the seventh port 116c of the second rotor 219 via a second duct/conduit 300b which comprises (i.e. extends through) the first heat exchanger 302a.
  • a first section 300b1 of duct 300b connects the sixth port 114d to the first heat exchanger 302a, and a second section 300b2 of duct 300b connects the first heat exchanger 302a to the seventh port 116c.
  • the fourth port 116b of the second rotor 219 is in fluid communication with the first port 114a of the first rotor 119 via a second duct/conduit 304a which comprises a second heat exchanger 306a.
  • the second heat exchanger 306a is operable to add heat energy to the working fluid passing through it (i.e. is a heat source ).
  • a first section 304a1 of duct 304a connects the fourth port 116b to the second heat exchanger 306a, and a second section 304a2 of duct 300a connects the second heat exchanger 306a to the first port 114a.
  • the eight port 116d of the second rotor 219 is in fluid communication with the fifth port 114c of the first rotor via a second duct/conduit 304b which comprises (i.e. extends through) the second heat exchanger 306a.
  • a first section 304b1 of duct 304b connects the eighth port 116d to the second heat exchanger 306a, and a second section 304b2 of duct 304b connects the second heat exchanger 306a to the fifth port 114c.
  • the first rotor 119 assembly i.e. the first rotor chambers 134a, 134b and first rotor pistons 122a, 122b
  • first housing 112 hence provide the first fluid flow section 111, which in this example are operable as a compressor or displacement pump.
  • the first fluid flow section 111 is configured for the passage of fluid between the first port 114a and second port 114b via the first rotor first chamber 134a, and for the passage of fluid between the fifth port 114c and sixth port 114d via the first rotor second chamber 134b.
  • the rotor 219 assembly i.e. second rotor chambers 234a, 234b and first rotor pistons 222a, 222b
  • second housing 212 hence provide the second fluid flow section 115, which in this example are operable as a metering section or expansion section.
  • the second fluid flow section 115 is configured for the passage of fluid between the third port 116a and fourth port 116b via the second rotor second chamber 234b, and for the passage of fluid between the seventh port 116c and eighth port 116d via the second rotor first chamber 234a,
  • the first chamber 134a and second chamber 134b of the first rotor 119 have substantially the same volumetric capacity as each other.
  • the first chamber 234a and second chamber 234b of the second rotor 219 i.e. the second fluid flow section 115
  • the volumetric capacity of the first rotor chambers 134a, 134b may be substantially the same, less, or greater than the volumetric capacity of the second rotor chambers 234a, 234b (second fluid flow section 115).
  • the volumetric capacity of the rotor chambers 234a, 234b of the second fluid flow section 115 may be the same, less, or greater than the volumetric capacity of the rotor chambers 134a, 134b first fluid flow section 111.
  • the volumetric capacity of the second fluid flow section 115 may be at most half the volumetric capacity of the first fluid flow section 111.
  • the volumetric capacity of the second fluid flow section 115 may be at least twice the volumetric capacity of the first fluid flow section 111.
  • the difference in volumetric capacity may be achieved by providing the first rotor chambers 134a, 134b as wider than the second rotor chambers 234a, 234b, with the first rotor pistons 122a, 122b consequentially being wider than the second rotor pistons 222a, 222b.
  • the pistons 122, 222 may pivot by the same angle, the volume of the first chambers 134a, 134b will be greater than the second chambers 234a, 234b, and the swept volume of the first rotor pistons 122a, 122b will be greater than the swept volume of the second rotor pistons 222a, 222b.
  • first rotor shaft 118 and second rotor shaft 218 are integrally formed as one, and extend through both rotors 119, 219.
  • the working fluid enters the sub-chambers 134a1, 134b1 via the first port 114a and fifth port 114c respectively.
  • the working fluid is then pumped (e.g. compressed) by the action of the respective pistons 122a, 122b driven by the motor 308, in the sub-chambers 134a, 134b and exits via the second port 114b and sixth port 114d respectively.
  • working fluid is being exhausted from the sub-chambers 134a1, 134b1, working fluid is being drawn into sub-chambers 134a2, 134b2 through the first port 114a and fifth port 114c respectively.
  • the working fluid travels along ducts 300a2, 300b2 and enters the sub-chambers 234b1, 234a1 of the second rotor via the third port 116a and seventh port 116c respectively where its pressure is restrained and the working fluid is metered into ducts 304a1, 304b1 respectively via the fourth port 116b and eighth port 116d respectively.
  • the working fluid is exhausted from the sub-chambers 234b1, 234a1 via the fourth port 116b and eighth port 116d, and more working fluid enters the sub-chambers 234b2, 234a2 via the third port 116a and seventh port 116c.
  • sequential delivery and behaviour of the working fluid in the rotor sub-chambers 234a1, 234a2, 234b1, 234b2 induces a force to thereby (at least in part) cause pivoting of the second rotor 219 about its second rotational axis 232, and to cause rotation of the rotor about its first rotational axis.
  • This force is in addition to that provided by the motor 308.
  • working fluid then travels from the second rotor chambers 234a, 234b along ducts 304a1, 304b1 and enters the second heat exchanger 306a, which in this example is configured as a heat source.
  • the working fluid absorbs heat from the heat source and then leaves the second heat exchanger 306a and travels along ducts 304a2, 304b2 before entering the first rotor chambers 134a, 134b to re-start the cycle.
  • Figure 19 illustrates an example of a closed loop heat engine (e.g.energy harvesting generator) apparatus 400 according to the present disclosure, which includes many features in common with, and potentially physically identical or equivalent to the example of Figure 15 , and which are hence referred to with the same reference numerals.
  • a closed loop heat engine e.g.energy harvesting generator
  • the example of Figure 19 differs from the example of Figure 15 in that, instead of a motor 308, a power off take 408 is coupled to, and driveable by the first shaft 118.
  • the power off take 408 may be provided as a coupling of a gear box for driving another device, for example an electrical generator.
  • first heat exchanger 302a is configured as a heat source (rather than the heat sink of Example 1) and second heat exchanger 306a is configured as a heat sink (rather than the heat source of Example 1). Otherwise, the Examples of Figures 15 , 19 are structurally the same.
  • thermodynamically reversible heat source and heat sink are provisioned and a motor 308 is provisioned which can also perform as a generator 408, that the same scheme may be thermodynamically reversible and perform both as a heat pump 100, or reverse and perform as a heat engine 400, in applications where such was seen as an advantage.
  • the sub-chambers 134a1, 134a2 which are operable as displacement/compression chambers in the Figure 15 example, are operable as expansion chambers in the Figure 19 example. That is to say, in this example the first chamber 134a and piston 122a (i.e. first fluid flow section 111) is operable as a fluid expansion section.
  • sub-chambers 134b1, 134b2 which are operable as metering/expansion chambers in the Figure 15 example, are operable as displacement/compression/pumping chambers in the Figure 19 example. That is to say, in the present example, the second chamber 134b and piston 122b (i.e. second fluid flow section 115) may be operable as a fluid displacement pump or, compressor.
  • expansion section i.e. first fluid flow section 111
  • displacement section i.e. second fluid flow section 115
  • the rotation of the rotor 119 is driven by the expansion of the working fluid in the first chamber 134a (i.e. in sub-chambers 134a1, 134a2).
  • the working fluid travels along duct 300a1 and enters the sub-chamber 134a2 of the rotor via the second port 114b where it expands.
  • the working fluid is exhausted from the sub-chamber 134a2 via the first port 114a, and more working fluid enters the sub-chamber 134a1 via the second port 114b where it expands.
  • sequential expansion of the working fluid in the rotor sub-chambers 134a1, 134a2 induces a force to thereby cause pivoting of the rotor about its second rotational axis 132, and to cause rotation of the rotor about its first rotational axis 130.
  • This rotational force drives the generator 408 via the shaft 118.
  • the working fluid enters the sub-chamber 134b2 via the fourth port 116b.
  • the working fluid is then displaced/pumped by the action of the piston 122b, driven by the expansion of the working fluid in the first chamber 134a, and exits via the third port 116a.
  • working fluid then travels from the second chamber 134b along duct 300a2 and enters the first heat exchanger 302a, which is configured as a heat source.
  • the working fluid absorbs heat from the heat source and then leaves the first heat exchanger 302a and travels along duct 300a1 before entering the first chamber 134a to re-start the cycle.
  • Figure 20 illustrates a second example of a closed loop heat engine (e.g. motor unit) apparatus 500 according to the present disclosure, which includes many features in common with, or equivalent to, the example of Figure 16 , and are hence referred to with the same reference numerals.
  • a closed loop heat engine e.g. motor unit
  • the example of Figure 20 differs from the example of Figure 16 in that, instead of a motor 308, a power off take 408 is coupled to, and driveable by the first shaft 118.
  • the power off take 408 may be provided as a coupling of a gear box for driving another device, for example an electrical generator.
  • first heat exchanger 302a is configured as a heat source (rather than the heat sink of Example 2) and second heat exchanger 306a is configured as a heat sink (rather than the heat source of Example 2). Otherwise, the Examples of Figures 16 , 20 are structurally the same.
  • first rotor sub-chambers 134a1, 134a2, 134b1, 134b2 which are operable as displacement/compression chambers in the Figure 16 example, are operable as expansion chambers in the Figure 20 example. That is to say, in this example the first rotor first chamber 134a and piston 122a, and first rotor second chamber 134b and second piston 122b (i.e. first fluid flow section 111) are operable as a fluid expansion section.
  • sub-chambers 234a1, 234a2, 234b1, 234b2 which are operable as expansion/metering chambers in the Figure 16 example, are operable as displacement/compression/pumping chambers in the Figure 20 example. That is to say, in the present example, second rotor first chamber 234a and piston 222a, and second rotor second chamber 234b and second piston 222b (i.e. second fluid flow section 115) may be operable as a fluid displacement pump or compressor.
  • the first chamber 134a and second chamber 134b of the first rotor 119 have substantially the same volumetric capacity as each other.
  • the first chamber 234a and second chamber 234b of the second rotor 219 i.e. the second fluid flow section 115
  • the volumetric capacity of the first rotor chambers 134a, 134b may be substantially the same, less, or greater than the volumetric capacity of the second rotor chambers 234a, 234b (second fluid flow section 115).
  • the volumetric capacity of the rotor chambers 234a, 234b of the second fluid flow section 115 may be the same, less, or greater than the volumetric capacity of the rotor chambers 134a, 134b first fluid flow section 111.
  • the volumetric capacity of the second fluid flow section 115 may be at most half the volumetric capacity of the first fluid flow section 111.
  • the volumetric capacity of the second fluid flow section 115 may be at least twice the volumetric capacity of the first fluid flow section 111.
  • the difference in volumetric capacity may be achieved by providing the first rotor chambers 134a, 134b as wider than the second rotor chambers 234a, 234b, with the first rotor pistons 122a, 122b consequentially being wider than the second rotor pistons 222a, 222b.
  • the pistons 122, 222 may pivot by the same angle, the volume of the first chambers 134a, 134b will be greater than the second chambers 234a, 234b, and the swept volume of the first rotor pistons 122a, 122b will be greater than the swept volume of the second rotor pistons 222a, 222b.
  • the working fluid travels along ducts 300a1, 300b1 and enters the sub-chambers 134a2, 134b2 respectively of the first rotor 119 via the second port 114b and sixth port 114d respectively where it expands.
  • the working fluid is exhausted from the sub-chamber 134a2, 134b2 via the first port 114a and fifth port 114c respectively, and more working fluid enters the sub-chambers 134a1, 134a2 via the second port 114b and sixth port 114d where it expands.
  • sequential expansion of the working fluid in the rotor sub-chambers 134a1, 134a2, 134b1, 134b2 induces a force to thereby cause pivoting of the first rotor about its second rotational axis 132, and to cause rotation of the first rotor 119 about its first rotational axis 130.
  • This rotational force drives the generator 408 via the shaft 118.
  • the working fluid enters the second rotor sub-chambers 234b2, 234a2 via the fourth port 116b eighth port 116d respectively.
  • the working fluid is then displaced/pumped by the action of the second rotor pistons 222a, 222b, driven by the expansion of the working fluid in the first rotor chambers 134a,134b and exits via the third port 116a and seventh port 116 respectively.
  • working fluid then travels from the second rotor second chambers 234b, 234a along ducts 300a2, 300b2 and enters the first heat exchanger 302a, which is configured as a heat source.
  • the working fluid absorbs heat from the heat source and then leaves the first heat exchanger 302a and travels along ducts 300a1, 300b1 before entering the first rotor first chambers 134a, 134b to re-start the cycle.
  • Figure 21 illustrates a first example of an open loop motor unit (heat engine) apparatus 600 according to the present disclosure, which includes many features in common, or equivalent to, the example of Figure 19 , and are hence referred to with the same reference numerals.
  • the system is an open loop, with no connection between the first port 114a and the fourth port 116b. That is to say, the second duct 304a and second heat exchanger 306a not present, and hence the first port 114a and the fourth port 116b are isolated from one another.
  • the fourth port 116b may be in fluid communication with a source of air, for example open to atmosphere.
  • the working fluid may comprise air.
  • the first heat exchanger 302a may comprise or be in thermal communication with any suitable heat source (for example solar heat, combustion exhaust or flue gases from another process, or steam).
  • the first heat exchanger 302a may comprise a combustion chamber 602 operable for continuous combustion.
  • the combustion chamber may include a burner supplied with a fuel to generate heat.
  • the combustion process may be a continuous combustion process.
  • the first heat exchanger 302a is a heat source configured to add heat energy to fluid passing through it.
  • the volumetric capacity of the first rotor second chamber 134b may be substantially the same, less, or greater than the volumetric capacity of the first rotor first chamber 134a.
  • the volumetric capacity of the second fluid flow section 115 may be the same, less, or greater than the volumetric capacity of the first fluid flow section 111.
  • the volumetric capacity of the first rotor second chamber 134b may be at most half the volumetric capacity of the first rotor first chamber 134a.
  • the volumetric capacity of the first rotor second chamber 134b may be at least twice the volumetric capacity of the first rotor first chamber 134a.
  • this provides an expansion ratio within the confines of a single device (for example as shown in Figure 17 ).
  • first rotor first chamber 134a as a different width than the first rotor second chamber 134b, with the first piston 122a consequentially having a different width than the second piston 122b.
  • the pistons will pivot, and hence travel, to the same extent around the second rotational axis 132, the volume of the chambers 134a, 134b and swept volume of the pistons 122a, 122b will differ.
  • the different volumes may be achieved by providing the first rotor first chamber 134a as wider than the first rotor second chamber 134b, with the first piston 122a consequentially being wider than the second piston 122b.
  • the pistons will pivot, and hence travel, to the same extent around the second rotational axis 132, the volume of the chamber 134a will be greater than the volume of chamber 134b, and hence the swept volume of the piston 122a will be greater than piston 122b.
  • the working fluid for example air
  • the working fluid enters the sub-chamber 134b2 via the fourth port 116b.
  • the working fluid is then displaced/compressed/metered by the action of the piston 122b, driven by expansion of working fluid in the first chamber 134a (described below in stage 3), and exits via the third port 116a.
  • working fluid then travels from the second chamber 134b along duct 300a2 and enters the first heat exchanger 302a, which is configured as a heat source.
  • the working fluid may be mixed with fuel in the combustor 603 to be in part burned and in part heated, increasing pressure, before being passed to the second port 114b of the expansion section, which in this example is the first fluid flow section 111.
  • the working fluid absorbs heat from the heat source and then leaves the first heat exchanger 302a and travels along duct 300a1 before entering the first chamber 134a.
  • the working fluid travels along duct 300a1 and enters the sub-chamber 134a2 of the rotor via the second port 114b where it expands.
  • the working fluid is exhausted from the sub-chamber 134a2 via the first port 114a, and more working fluid enters the sub-chamber 134a1 via the second port 114b where it expands.
  • the exhaust gas expands sequentially in the sub-chambers 134a1, 134a2 of the first chamber 134a (hence the gas decreases in pressure and increases in volume), so that work is done by the gas on the first piston 122a to urge the first piston 122a across the chamber 134a (operating as an expansion chamber), which drives the second piston 122b across the second chamber 134b to draw in and compress a further portion of air to start the process again.
  • Figure 22 illustrates a second example of an open loop motor unit (heat engine) apparatus 700 according to the present disclosure, which includes many features in common with, or equivalent to, the example of Figure 20 , and are hence referred to with the same reference numerals.
  • the system is an open loop, with no connection between the second rotor flow inlets (which in this example are the fourth port 116b and eighth port 116d) the first rotor flow outlets (which in this example are the first port 114c and fifth port 114c) respectively. That is to say, the second duct 304a and second heat exchanger 306a of Example 4 ( Figure 20 ) are not present in the example of Figure 22 , and hence the fourth port 116b and first port 114a are isolated from one another, and the eighth port 116d and fifth port 114c are isolated from one another.
  • the fourth port 116b and eight port 116d may be in fluid communication with a source of air, for example open to atmosphere.
  • the working fluid may comprise air.
  • the first heat exchanger 302a may comprise or be in thermal communication with any suitable heat source (for example solar heat, combustion exhaust or flue gases from another process, or steam).
  • the first heat exchanger 302a may comprise a combustion chamber 602 operable for continuous combustion.
  • the combustion chamber may include a burner supplied with a fuel to generate heat.
  • the combustion process may be a continuous combustion process.
  • the first heat exchanger 302a is operable to add heat energy to fluid passing through it.
  • combustion chamber 602a, 602b for each fluid circuit.
  • the chambers 602a, 602b may be fluidly isolated from one another. Hence a first combustion chamber 602a may be provided in fluid communication with duct 300a, and a second combustion chamber 602b may be provided in fluid communication with duct 300b.
  • the combustion chambers 602a, 602b may be provided within a single combustion chamber unit 602.
  • the working fluid for example air
  • the working fluid enters the second rotor sub-chambers 234b2, 234a2 via the fourth port 116b and eight port 116d respectively.
  • the working fluid is then displaced/compressed/metered by the action of the second rotor pistons 222a, 222b, driven by expansion of working fluid in the first rotor first chambers 134a, 134b (described below in stage 3), and exits via the third port 116a and seventh port 116c respectively.
  • working fluid is being drawn into sub-chambers 234b1, 234a1 through the fourth port 116b and eight port 116d respectively.
  • working fluid then travels from the second rotor second chambers 234b, 234a along ducts 300a2, 300b2 and enters the first heat exchanger 302a, which is configured as a heat source.
  • the working fluid may be mixed with fuel in the combustor 603 to be in part burned and in part heated, increasing pressure, before being passed to the second port 114b and sixth port 114d of the first rotor 119 (i.e. the first fluid flow section 111, or "expansion" section).
  • the working fluid absorbs heat from the heat source and then leaves the first heat exchanger 302a and travels along ducts 300a1, 300b1 before entering the first rotor chambers 134a, 134b.
  • the working fluid travels along ducts 300a1, 300b1 and enters the sub-chambers 134a2, 134a2 of the first rotor 119 via the second port 114b and sixth port 114d where it expands.
  • the working fluid is exhausted from the sub-chambers 134a2, 134b2 via the first port 114a and fifth port 114c, and more working fluid enters the sub-chambers 134a1, 134b1 via the second port 114b and sixth port 114d where it expands.
  • the exhaust gas expands sequentially in the sub-chambers 134a1, 134a2, 134b1, 134b2 of the first rotor chambers 134a, 134b (hence the gas decreases in pressure and increases in volume), so that work is done by the gas on the first rotor pistons 122a, 122b to urge the first piston 122a across the chamber 134a (operating as an expansion chamber) and to urge the second piston 122b across the chamber 134b (operating as an expansion chamber), which drives the first and second pistons 122a, 122b across their respective chambers 134a, 134b to draw in a further portion of air to start the process again.
  • Figure 23 illustrates a third example of an open loop heat engine (motor unit) apparatus 800 according to the present disclosure, which includes many features in common with, or equivalent to, the example of Figure 21 , and are hence referred to with the same reference numerals.
  • the fourth port 116b is configured to be in fluid communication with a source of hot gas, for example flue or exhaust gas.
  • a source of hot gas for example flue or exhaust gas.
  • the working fluid may comprise a source of hot gas, for example flue or exhaust gas.
  • the first heat exchanger 302a comprises a chamber 810 operable to permit fluid flow between the displacement section (in this example the second fluid flow section 115) and the expansion section (in this example the first fluid flow section 111), and an injector 812 is configured to inject a cryogenic medium into the chamber 810 such that heat energy is transferred from the fluid to the cryogenic media to cause it to increase in pressure.
  • the first heat exchanger 302a is operable to remove heat energy from working fluid passing through it in return for an increase in pressure of the cryogenic medium, and is thus configured as a heat sink.
  • the cryogenic fluid may be a gas in normal atmospheric conditions stored in a compressed liquid or state, which requires heat input during its phase change back to a gas, for example liquid nitrogen or liquid air.
  • a gas for example liquid nitrogen or liquid air.
  • 'cryogenic fluid' is intended to mean any medium stored in a low temperature liquid or gas state which will expand, perhaps aggressively, with introduction of heat.
  • the volumetric capacity of the first rotor second chamber 134b may be substantially the same, less, or greater than the volumetric capacity of the first rotor first chamber 134a.
  • the volumetric capacity of the second fluid flow section 115 may be the same, less, or greater than the volumetric capacity of the first fluid flow section 111.
  • the volumetric capacity of the first rotor second chamber 134b may be at most half the volumetric capacity of the first rotor first chamber 134a.
  • the volumetric capacity of the first rotor second chamber 134b may be at least twice the volumetric capacity of the first rotor first chamber 134a.
  • this provides an expansion ratio within the confines of a single device (for example as shown in Figure 17 ).
  • first rotor first chamber 134a as a different width than the first rotor second chamber 134b, with the first piston 122a consequentially having a different width than the second piston 122b.
  • the pistons will pivot, and hence travel, to the same extent around the second rotational axis 132, the volume of the chambers 134a, 134b and swept volume of the pistons 122a, 122b will differ.
  • the different volumes may be achieved by providing the first rotor first chamber 134a as wider than the first rotor second chamber 134b, with the first piston 122a consequentially being wider than the second piston 122b.
  • the pistons will pivot, and hence travel, to the same extent around the second rotational axis 132, the volume of the chamber 134a will be greater than the volume of chamber 134b, and hence the swept volume of the piston 122a will be greater than piston 122b.
  • the working fluid enters the sub-chamber 134b2 via the fourth port 116b.
  • the working fluid is then displaced/metered by the action of the piston 122b, driven by expansion of working fluid in the first chamber 134a (described below), and exits via the third port 116a.
  • working fluid then travels from the second chamber 134b along duct 300a2 and enters the first heat exchanger 302a, which is configured as a heat sink.
  • the hot gas may be mixed with the cryogenic medium in the chamber 810 such that heat is transferred to the cryogenic medium causing it to increase in pressure before being passed to the second port 114b of the expansion section (in this example, the first fluid flow section 111).
  • cryogenic medium is mixed with, and absorbs heat from, the working fluid and then leaves the first heat exchanger 302a and travels along duct 300a1 before entering the first chamber 134a.
  • the working fluid travels along duct 300a1 and enters the sub-chamber 134a2 of the rotor via the second port 114b where it expands.
  • the working fluid is exhausted from the sub-chamber 134a2 via the first port 114a, and more working fluid enters the sub-chamber 134a1 via the second port 114b where it expands.
  • Figure 24 illustrates a fourth example of an open loop heat engine motor unit apparatus 900 according to the present disclosure, which includes many features in common with, or equivalent to, the example of Figure 22 , and are hence referred to with the same reference numerals.
  • the example of Figure 24 differs from the example of Figure 22 in that the second rotor flow inlets (which in this example are the fourth port 116b and eighth port 116d are configured to be in fluid communication with a source of hot gas, for example flue or exhaust gas.
  • a source of hot gas for example flue or exhaust gas.
  • the working fluid may comprise a source of hot gas, for example flue or exhaust gas.
  • first chamber 134a and second chamber 134b of the first rotor 119 have substantially the same volumetric capacity (i.e. the same volume) as each other.
  • the first chamber 234a and second chamber 234b of the second rotor 219 i.e. the second fluid flow section 115
  • volumetric capacity (i.e volume) of the first rotor chambers 134a, 134b (first fluid flow section 111) may be substantially the same, less, or greater than the volumetric capacity (i.e. volume) of the second rotor chambers 234a, 234b (second fluid flow section 115).
  • the volumetric capacity (i.e. volume) of the rotor chambers 234a, 234b of the second fluid flow section 115 may be the same, less, or greater than the volumetric capacity (i.e. volume) of the rotor chambers 134a, 134b first fluid flow section 111.
  • the volumetric capacity of the second fluid flow section 115 may be at most half the volumetric capacity of the first fluid flow section 111.
  • the volumetric capacity of the second fluid flow section 115 may be at least twice the volumetric capacity of the first fluid flow section 111.
  • the first heat exchanger 302a comprises a chamber 810 operable to permit fluid flow between the displacement section (in this example the second rotor 219, i.e. the second fluid flow section 115) and the expansion section (in this example the first rotor 119, i.e. the first fluid flow section 111), and an injector 812 is configured to inject a cryogenic medium into the chamber 810 such that heat energy is transferred from the fluid to the cryogenic media to cause it to increase in pressure.
  • the first heat exchanger 302a is operable to remove heat energy from working fluid passing through it in return for an increase in pressure of the cryogenic medium, and is thus configured as a heat sink.
  • a mixing chamber 810a, 810b and injector 812 for each fluid circuit.
  • the chambers 810a, 810b may be fluidly isolated from one another. Hence a first cryogenic chamber 810a may be provided in fluid communication with duct 300a, and a second cryogenic chamber 810b may be provided in fluid communication with duct 300b.
  • the mixing chambers 810a, 801b may be provided within a single mixing chamber unit 810.
  • the working fluid enters the second rotor sub-chambers 234b2, 234a2 via the fourth port 116b and eight port 116d respectively.
  • the working fluid is then displaced/compressed/metered by the action of the second rotor pistons 222a, 222b, driven by expansion of working fluid in the first rotor first chambers 134a, 134b (described below in stage 3), and exits via the third port 116a and seventh port 116c respectively.
  • working fluid is being drawn into sub-chambers 234b1, 234a1 through the fourth port 116b and eight port 116d respectively.
  • working fluid then travels from the second rotor second chambers 234b, 234a along ducts 300a2, 300b2 and enters the first heat exchanger 302a, which is configured as a heat sink.
  • the hot gas may be mixed with the cryogenic medium in the mixing chamber 810 such that heat is transferred to the cryogenic medium causing it to increase in pressure before being passed to the second port 114b and sixth port 114d of the first rotor 119 (i.e. the first fluid flow section 111, or "expansion" section).
  • cryogenic medium is mixed with, and absorbs heat from, the working fluid and then leaves the first heat exchanger 302a and travels along ducts 300a1, 300b1 before entering the first rotor chambers 134a, 134b.
  • the working fluid travels along ducts 300a1, 300b1 and enters the sub-chambers 134a2, 134a2 of the first rotor 119 via the second port 114b and sixth port 114d where it expands.
  • the working fluid is exhausted from the sub-chambers 134a2, 134b2 via the first port 114a and fifth port 114c, and more working fluid enters the sub-chambers 134a1, 134b1 via the second port 114b and sixth port 114d where it expands.
  • the exhaust gas expands sequentially in the sub-chambers 134a1, 134a2, 134b1, 134b2 of the first rotor chambers 134a, 134b (hence the gas decreases in pressure and increases in volume), so that work is done by the gas on the first rotor pistons 122a, 122b to urge the first piston 122a across the chamber 134a (operating as an expansion chamber) and to urge the second piston 122b across the chamber 134b (operating as an expansion chamber), which drives the first and second pistons 122a, 122b across their respective chambers 134a, 134b to draw in a further portion of air to start the process again.
  • the first rotor first chamber 134a may have a volumetric capacity substantially less than or substantially greater than the volumetric capacity of the first rotor second chamber 134b.
  • the second rotor second chamber 234b may have a volumetric capacity substantially less than or substantially greater than the volumetric capacity of the second rotor first chamber 234a.
  • first rotor first chamber 134a may have a volumetric capacity of at most half or at least twice the volumetric capacity of the first rotor second chamber 134b.
  • second rotor second chamber 234b may have a volumetric capacity of at most half or at least twice the volumetric capacity of the second rotor first chamber 234a.
  • Such an example provides a multi stage device, or two working fluid circuits with different expansion ratios through a common system.
  • Ducts 300a, 300b and ducts 304a, 304b have been illustrated as discrete circuits. However duct 300a and duct 300b may, at least in part, be combined to define a common flow path which passes through heat exchanger 302. Likewise duct 304a and duct 304b may, at least in part, be combined to define a common flow path which passes through heat exchanger 306. Alternatively the ducts 300a, 300b may pass through entirely separate heat exchanger units 302 having different, or the same, heat capacities as each other. Likewise alternatively the ducts 304a, 304b may pass through entirely separate heat exchanger units 306 having different, or the same, heat capacities as each other.
  • drive shafts 118, 218 are described as being rigidly/directly linked and so they operate at the same rotational speed as each other to provide lossless operation between them.
  • first shaft 118 and second shaft 218 may be coupled by mechanical (for example by a gear box) or virtual means (for example by an electronic control system) so they may rotate at different speeds relative to one another.
  • the core of the apparatus of the present disclosure is a true positive displacement unit which offers up to a 100% internal volume reduction per revolution. It is operable to simultaneously 'push' and 'pull' the piston 122 across its chamber, so for example, in the same chamber can create a full vacuum on one side of a piston whilst simultaneously producing compression and/or displacement on the other.
  • Coupling of the displacement section and expansion sections i.e. direct drive between the first fluid flow section 111 and second fluid flow section 115, whether part of the same rotor as shown in Figures 15 , 19 , 21 , 23 or linked rotors as shown in Figures 16 , 20 , 22 , 24 ) means that mechanical losses are minimised relative to examples of the related art, as well as enabling recovery from the processes in each section to help drive the other side.
  • the device can perform efficient operation under varied loads and varied speeds, which is not possible with a conventional arrangement (for example those including an axial flow turbine). This allows for harvesting of energy at input levels not previously achievable.
  • the apparatus of the present invention can be scaled to any size to suit different capacities or power requirements, its dual output drive shaft also makes it easy to mount multiple drives on a common line shaft, thereby increasing capacity, smoothness, power output, offering redundancy, or more power on demand.
  • a heat engine device of the present disclosure could be carried on a vehicle to provide additional drive or electrical generation to supplement the output of a larger engine with little weight penalty.
  • the device inherently has an extremely low inertia which offers low load and quick and easy start-up.
  • the apparatus of the present disclosure provides a technical solution with a high thermodynamic efficiency, which can operate at low speed. Operation at low speed is advantageous as it enables electricity generation at speeds closer to or at the required frequency, thereby reducing reliance, and losses due to, gearing and signal inversion.
  • the rotor 14 and housing 12 may be configured with a small clearance between them thus enabling oil-less and vacuum operation, and/or obviate the need for contact sealing means between rotor 16 and housing 12, thereby minimising frictional losses.
  • the shaft 18, 118, 218 may extend out of both sides of the rotor housing to be coupled to a powertrain for driving device and/or an electrical generator.
  • Figure 25 illustrates an example of an open loop air cycle apparatus 1000 according to the present disclosure, which includes many features in common, or equivalent to, the example of Figure 21 , and are hence referred to with the same reference numerals.
  • the system is an open loop, with no connection between the first port 114a and the fourth port 116b. That is to say, the second duct 304a and second heat exchanger 306a not present, and hence the first port 114a and the fourth port 116b are isolated from one another.
  • a motor 308 is coupled to the first shaft portion 118 to drive the rotor 119 around the first rotational axis 130.
  • the first chamber 134a and piston 122a hence provide a first fluid flow section 111, which in this example are operable as a compressor or displacement pump.
  • the first fluid flow section 111 is configured for the passage of fluid between the first port 114a and second port 114b via the first chamber 134a.
  • the second chamber 134b and piston 122b hence provide a second fluid flow section 115, which in this example are operable as a metering section or expansion section.
  • the second fluid flow section 115 is configured for the passage of fluid between the third port 116a and fourth port 116b via the second chamber 134.
  • the first port 114a may be in fluid communication with a source of ambient air, for example open to atmosphere.
  • the working fluid may comprise air.
  • the fluid may be any suitable fluid.
  • the first heat exchanger 302a may be in thermal communication with any suitable heat source or a substance to be cooled.
  • a substance for example a second fluid to be cooled, is passed through a duct 303 in the first heat exchanger 302a, such that the substance may transfer heat to the working fluid and the substance is cooled as it passes through the first heat exchanger 302.
  • the substance may be any medium that may flow and be cooled, such as a fluid such as air, gas or liquid.
  • the substance is medium for cooling personal climatic conditions, for example to provide temperature control in buildings.
  • the substance may be used to cool or heat electronics systems.
  • the first heat exchanger 302a is a heat source configured to add heat energy to working fluid passing through it.
  • the volumetric capacity of the first chamber 134a may be substantially the same, less, or greater than the volumetric capacity of the second chamber 134b.
  • the volumetric capacity of the second fluid flow section 115 may be the same, less, or greater than the volumetric capacity of the first fluid flow section 111.
  • the volumetric capacity of the second fluid flow section 115 is preferably greater than the volumetric capacity of the first fluid flow section 111.
  • volumetric capacity of the second chamber 134b may be at most half the volumetric capacity of the first rotor first chamber 134a.
  • the volumetric capacity of the second chamber 134b may be at most 20% of the volumetric capacity of the first rotor first chamber 134a
  • the volumetric capacity of the first rotor second chamber 134b may be at least twice the volumetric capacity of the first rotor first chamber 134a.
  • volumetric capacity of the first rotor second chamber 134b may be at least three times the volumetric capacity of the first rotor first chamber 134a.
  • this provides an expansion ratio within the confines of a single device (for example as shown in Figure 17 ).
  • first chamber 134a as a different width than the second chamber 134b, with the first piston 122a consequentially having a different width than the second piston 122b.
  • the pistons will pivot, and hence travel, to the same extent around the second rotational axis 132, the volume of the chambers 134a, 134b and swept volume of the pistons 122a, 122b will differ.
  • the different volumes may be achieved by providing the second chamber 134b as wider than the first chamber 134a, with the second piston 122b consequentially being wider than the first piston 122a.
  • the volume of the second chamber 134b will be greater than the volume of the first chamber 134a, and hence the swept volume of the piston 122b will be greater than piston 122a.
  • first fluid flow section 111 in this example a displacement/compressor/pump section
  • second fluid flow section 115 in this example a metering/expansion section
  • the rotation of the rotor 119 is driven both by the motor and the metering/expansion of the fluid in the second chamber 134b (i.e. in sub-chambers 134b1, 134b2).
  • the working fluid for example air enters the sub-chamber 134a1 via the first port 114a.
  • the working fluid is then displaced/compressed/metered by the action of the piston 122a, driven by the motor 308 and the expansion of working fluid in the second chamber 134b (described below in stage 3), and exits via the second port 114b.
  • working fluid is being drawn into the sub-chamber 134a1, working fluid is being exhausted from sub-chamber 134a2 through the second port 114b.
  • the working fluid then travels from the first chamber 134a along duct 300a1 and enters the first heat exchanger 302a, which is configured as a heat source. Hence heat is added to the working fluid as it passes through the first heat exchanger 302a.
  • a substance such as air, gas or liquid may also be passed through the heat exchanger 302a, via a separate inlet and acts to transfer heat to the working fluid.
  • a substance enters the heat exchanger 302a at a first temperature and leaves the heat exchanger at a second temperature, wherein the second temperature is lower than the first temperature.
  • the heat from the substance is transferred to the working fluid.
  • the working fluid absorbs heat from the heat source (for example, the substance) and then leaves the first heat exchanger 302a and travels along duct 300a2 before entering the second chamber 134b.
  • the working fluid exits the first heat exchanger 302a via the duct 300a2.
  • the pressure of the working fluid is held at a relatively low pressure in the duct 300a2, for example below atmospheric pressure.
  • the working fluid travels along duct 300a2 and enters the sub-chamber 134b1 of the rotor via the third port 116a and the working fluid is expanded.
  • working fluid is entering and expanding in the sub-chamber 134b1, working fluid is being exhausted from sub-chamber 134b2 via the fourth port 116b.
  • the working fluid is exhausted from the sub-chamber 134b2 via the fourth port 116b, and more working fluid enters the sub-chamber 134b1 via the third port 116a where it expands.
  • the exhaust gas expands sequentially in the sub-chambers 134b1, 134b2 of the second chamber 134b (hence the fluid decreases in pressure and increases in volume).
  • this expansion results in a negative pressure being maintained in the duct 300a, which in turn contributes to driving the first piston 122a across chamber 134a introducing a further portion of air to start the process again.
  • the expansion of the exhaust gas in sub-chambers 134b1, 134b2 may result in work being done by the fluid on the second piston 122b to urge the first piston 122b across the chamber 134b (operating as an expansion chamber), which drives the first piston 122a across the first chamber 134a to draw in and compress a further portion of air to start the process again.
  • the system shown in Figure 25 is operable to work as an air source cold pump.
  • the system of Figure 25 is reversible such that if the direction of the motor 308 is reversed, a positive pressure difference is created between the second fluid flow section 115 and the first fluid flow section 111.
  • the heat exchanger 302 extracts heat from the fluid passing therethrough to heat a substance in duct 303.
  • the system is an air source heat pump.
  • the motor 308 may be reversible.
  • the motor 308 is configured to drive the rotor 119 around the first rotational axis 130 in a first direction
  • the first heat exchanger 302a is operable to act as a heat source to transfer heat from the substance to the fluid.
  • the first heat exchanger 302a is operable to act as a heat source to transfer heat from the fluid to the substance.
  • the system to operable to work as an air source heat pump.
  • Figure 26 shows a part exploded view of an alternative example of a core 510 forming part of an apparatus according to the present disclosure.
  • the core 510 comprises a housing 512 and rotor assembly 514.
  • Figures 27A and 27B shows a side view and cross-sectional example of the housing 512 when it is closed around the rotor assembly 514.
  • the housing 512 is divided into three parts 512a, 512b and 512c which close around the rotor assembly 14.
  • the housing may be fabricated from more than two parts, and/or split differently to that shown in Figure 26 .
  • the housing 512 comprises a first housing end 512a and a second housing end 512b, which may be coupled to a spacer ring 512c in use.
  • the first housing end 512a and the second housing end 512b may be clamped to the spacer ring 512c.
  • the outer race of a bearing 529 is coupled to the spacer ring 512c.
  • the outer race of a bearing is formed on the inner surface of the spacer ring 512c or housing 512.
  • the piston member 522 and the axle 520 are substantially identical to the piston member 22 and the axle 20 shown in Figures 8 to 10 .
  • one or more bearings 521 may be provided on the rotor 516 to enable the axle 520 to rotate relative to the rotor 516.
  • a bearing pin 523 may be placed in the one or more bearings 521 to axially fix the axle 520 relative to the rotor 516, whilst enabling rotational movement about the axis 532.
  • a cap 525 may be placed over the bearing pin 523 and bearing 521.
  • the orbital slewing ring comprises a first ring 527A and a second ring 527B configured to couple with the inner race of a bearing 529.
  • the first ring 527A and a second ring 527B are configured to be clamped together to clamp at least part of the bearing 529 therebetween.
  • the first guide feature (552) may comprise a stylus configured to be received in or coupled with the slewing ring (527).
  • the second guide feature 550 comprises the orbital slewing ring 527A, 527B, and the bearing 529, which may be made up of inner race, outer race and rolling element.
  • a first guide feature 552 may be mechanically coupled with the second guide feature 550.
  • the first guide feature 552 comprises a stylus configured to be received in the orbital slewing ring 527 so as to couple the rotor 516 to the orbital slewing ring 527A, 527B.
  • the bearing 529 forms a guide path to pivot the rotor 516 relative to the shaft 522 around axis 530.
  • the guide path resulting from the coupling of the first guide feature 552 and the second guide feature 550 may describe a path around (i.e. on, close to, and/or to either side of) a first circumference of the housing 512.
  • the provision of the bearing track formed from the first guide feature 552 and the second guide feature 550 reduces the friction and noise, vibration and harshness in the apparatus.
  • Bearing 529 may be in any form, ie with rolling, ball or other frictionless element or of a plain bearing type. The example shown is an angular contact back to back ball bearing pair.
  • a back to back pair of angular contact bearings offers a higher speed tolerance, higher load tolerance, larger rolling element, track load is spread over a larger area rather than a single point.
  • the bearing can be used to hold the rotor 516 on centre within the housing 512 so thermal growth is equal in each direction away from the centre point.
  • the trend of the guide path defines a ramp, amplitude and frequency of the rotor 516 about the second rotational axis 532 in relation to the rotation of the first rotational axis 530, thereby defining a ratio of angular displacement of the chambers 534 in relation to the radial reward from the shaft (or vice versa) at any point.
  • attitude of the path directly describes the mechanical ratio/relationship between the rotational velocity of the rotor and the rate of change of volume of the rotor chambers 534a, 534b. That is to say, the trajectory of the path 550 directly describes the mechanical ratio/relationship between the rotational velocity of the rotor 516 and the rate of pivot of the rotor 516.
  • the guide path , resulting from the coupling of the first guide feature 552 and the second guide feature 550 is at a 30 degree angle to vertical, in other examples this angle may differ.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Hydraulic Motors (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Soil Working Implements (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)
EP19707079.0A 2018-02-27 2019-02-15 Roticulating thermodynamic apparatus Active EP3755884B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP22159775.0A EP4056804A1 (en) 2018-02-27 2019-02-15 Roticulating thermodynamic apparatus

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB1803181.5A GB2571354B (en) 2018-02-27 2018-02-27 Roticulating thermodynamic apparatus
PCT/GB2019/050402 WO2019166769A1 (en) 2018-02-27 2019-02-15 Roticulating thermodynamic apparatus

Related Child Applications (2)

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EP22159775.0A Division-Into EP4056804A1 (en) 2018-02-27 2019-02-15 Roticulating thermodynamic apparatus
EP22159775.0A Division EP4056804A1 (en) 2018-02-27 2019-02-15 Roticulating thermodynamic apparatus

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EP3755884A1 EP3755884A1 (en) 2020-12-30
EP3755884B1 true EP3755884B1 (en) 2022-04-13

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EP19707079.0A Active EP3755884B1 (en) 2018-02-27 2019-02-15 Roticulating thermodynamic apparatus
EP22159775.0A Pending EP4056804A1 (en) 2018-02-27 2019-02-15 Roticulating thermodynamic apparatus

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Country Status (15)

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US (2) US11085301B2 (ru)
EP (3) EP3755883B1 (ru)
JP (1) JP6922100B2 (ru)
CN (1) CN111919012B (ru)
AU (1) AU2019226434B2 (ru)
CA (2) CA3091765C (ru)
CL (1) CL2020002176A1 (ru)
GB (1) GB2571354B (ru)
IL (1) IL276769B (ru)
NZ (1) NZ767494A (ru)
RU (1) RU2752114C1 (ru)
SG (1) SG11202007895PA (ru)
UA (1) UA125054C2 (ru)
WO (2) WO2019166768A1 (ru)
ZA (1) ZA202005111B (ru)

Families Citing this family (2)

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GB201520830D0 (en) * 2015-11-25 2016-01-06 Fenton Jonathan P Fluid compression apparatus
GB2611027B (en) * 2021-09-17 2023-09-27 Fetu Ltd Thermodynamic cycle

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Publication number Publication date
AU2019226434A1 (en) 2020-09-17
US20200400023A1 (en) 2020-12-24
SG11202007895PA (en) 2020-09-29
US10989053B2 (en) 2021-04-27
CA3091763C (en) 2021-10-19
GB2571354B (en) 2020-04-15
WO2019166769A1 (en) 2019-09-06
US11085301B2 (en) 2021-08-10
EP3755883B1 (en) 2022-04-13
RU2752114C1 (ru) 2021-07-22
IL276769B (en) 2021-04-29
CA3091765C (en) 2021-04-06
JP2021508800A (ja) 2021-03-11
GB201803181D0 (en) 2018-04-11
NZ767494A (en) 2023-03-31
UA125054C2 (uk) 2021-12-29
GB2571354A (en) 2019-08-28
CA3091765A1 (en) 2019-09-06
EP3755884A1 (en) 2020-12-30
IL276769A (en) 2020-10-29
EP3755883A1 (en) 2020-12-30
AU2019226434B2 (en) 2021-05-20
WO2019166768A1 (en) 2019-09-06
ZA202005111B (en) 2022-01-26
JP6922100B2 (ja) 2021-08-18
CN111919012B (zh) 2021-07-27
EP4056804A1 (en) 2022-09-14
US20200408096A1 (en) 2020-12-31
CA3091763A1 (en) 2019-09-06
CL2020002176A1 (es) 2020-11-13
CN111919012A (zh) 2020-11-10

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